Cessna Model 152 aircraft is high-wing monoplanes of all-metal semimonocoque construction and are equipped with fixed tubular spring-steel main gear struts and a steerable nose gear. The nose gear has an air/hydraulic fluidshook strut. Two-place seating is standard, and a double-width, fold-up auxiliary rear seat is optional. Also featured is a "wrap-around" rear window and a sweptback fin and rudder. Powering these aircraft is a four-cylinder. horizontally-opposed air cooled Lycoming "Blue Streak" engine, driving an all-metal fixed-pitch propeller.
GROSS WEIGHT (Takeoff or Landing) .........................1670 Lbs.
FUEL CAPACITY Standard Wing (Total) ......................22.6 Gal
Standard Wing (Usable) ............................................ ...245 Gal.
Long Range Wing (Total) ........................................... ..39 Gal
Long Range Wing (Usable) .................................... .. ..37.5 Gal
OIL CAPACITY Without External Filter .............. 6 Qt.
With External Filter ................. 7 Qt.
ENGINE MODEL .......................................................... ...Lycoming 0-235 Series
PROPELLER (Fixed Pitch) ..................................... .......69" McCauley
MAIN WHEEL TIRES (Optional) ........................... ....... 6.00 x 6, 4-Ply Rating
Pressure ............................ ...21 Psi
MAIN WHEEL TIRES (Standard) ........................... ........ 15 x 600 x 6, 4-Ply Rating
Pressure ......... ...... ......... ...29 Psi
NOSE WHEEL Tire (Standard) ............................... ........5.00 x 5, 4-Ply Rating
Pressure ..................... ... 30 Psi
NOSE GEAR STRUT PRESSURE (Strut Extended)...... 20 Psi
WHEEL ALIGNMENT Camber ..................... ................... 3 to +5 °
Toe-in ............................ .... 0" to + .16"
AILERON TRAVEL Up ....................................... 20° + 2° - 0
Down .......................... : .... 15° + 2° - 0
Droop ..... ......................... + 11°/2 ° Down from streamline
WING FLAP TRAVEL .......................................... .............30° 2° Down
RUDDER TRAVEL (Parallel to Water Line)
Right ............................... 20° 30' +0 -2°
Left ....... ..........................20 30' +0° -2 °
RUDDER TRAVEL (Perpendicular to Hinge Line)
Right ................................. 23, +00 -20'
Left .................................... 23°, +0 -2
ELEVATOR TRAVEL Up ...........25° 1° Down ... 18° + 1°
ELEVATOR TRIM TAB Up................ 10 ° 1 Down ..... 20° 1°
PRINCIPAL DIMENSIONS
Wing Span ........... ................................................... 400.00"
Length ..................................... ................................. 284.84"
Fin Height (Maximum With Nose Gear Depressed And
Flashing Beacon Installed on Fin) ...................... 102.00"
Track Width ................................................................ 91.28"
Tail Span ..................................................................... 120.00"
BATTERY LOCATION .................................. FIREWALL Right Side
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